Federal Aviation Administration April 2014 – Federal Register Recent Federal Regulation Documents

The Federal Aviation Administration (FAA) is issuing this notice to advise the public that the Draft Written Reevaluation for a minor adjustment to a project evaluated in FAA's 2005 Final Environmental Impact Statement (FEIS) for the LAX Master Plan will be made available for public comment. The Draft Written Reevaluation has been prepared for the construction and operation of the proposed West Aircraft Maintenance Area (WAMA) west of Taxiway AA in the southwest quadrant of Los Angeles International Airport, Los Angeles, California. FAA is seeking comments on the Draft Written Reevaluation.

The FAA is issuing this notice to advise the public of the fifth meeting of the RTCA Tactical Operations Committee.

This notice contains a summary of a petition seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of the petition or its final disposition.

This rule amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.

This rule establishes, amends, suspends, or revokes Standard Instrument Approach Procedures (SIAPs) and associated Takeoff Minimums and Obstacle Departure Procedures for operations at certain airports. These regulatory actions are needed because of the adoption of new or revised criteria, or because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, adding new obstacles, or changing air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports.

In accordance with the Paperwork Reduction Act of 1995, FAA invites public comments about our intention to request from the Office of Management and Budget (OMB) approval to renew an information collection. The Federal Register Notice with a 60-day comment period soliciting comments on the following collection of information was published on February 11, 2014, vol. 79, no. 28, pages 8231-8232. The FAA requires that certain performance information be provided in the Rotorcraft Flight Manual in order to show compliance to the regulatory requirements. The flight manual, by regulation, must be furnished with each aircraft.

We are superseding Airworthiness Directive (AD) 2014-03-08 for all Airbus Model A318, A319, A320, and A321 series airplanes. AD 2014- 03-08 required an inspection to determine the part number of the interconnecting struts installed on the wings, identifying the part number and the serial number of the associated target and proximity sensor if applicable, and replacing or re-identifying the flap interconnecting strut if applicable. This new AD corrects a typographical error that affects the definition of a serviceable interconnecting strut. This AD was prompted by a report that an investigation showed that when a certain combination of a target/ proximity sensor serial number is installed on a flap interconnecting strut, a ``target FAR'' signal cannot be detected when it reaches the mechanical end stop of the interconnecting strut. We are issuing this AD to detect and correct a latent failure of the flap down drive disconnection due to an already-failed interconnecting strut sensor, which could result in asymmetric flap panel movement and consequent loss of control of the airplane.

We are adopting a new airworthiness directive (AD) for certain Airbus Model A330-200 and -300 series airplanes, and Model A340-200 and -300 series airplanes. This AD requires repetitive inspections of certain sidestay upper cardan pins of the main landing gear (MLG), and associated nuts and retainer assemblies, and pin replacement if necessary. This AD also provides for an optional measurement of the cardan pin clearance dimensions (gap check) and corrective actions if necessary, which would terminate the repetitive inspections. This AD was prompted by a report of a sidestay upper cardan pin of the MLG migrating out of position. We are issuing this AD to detect and correct migration of the sidestay upper cardan pin, which could result in disconnection of the sidestay upper arm from the airplane structure, and could result in a landing gear collapse and consequent damage to the airplane and injury to occupants.

We are superseding Airworthiness Directive (AD) 2009-24-07 for certain the Boeing Company Model 737-600, -700, -700C, and -800 series airplanes. AD 2009-24-07 required repetitive lubrications of the right and left main landing gear (MLG) forward trunnion pins. AD 2009-24-07 also required an inspection for discrepancies of the transition radius of the MLG forward trunnion pins, and corrective actions if necessary. For certain airplanes, AD 2009-24-07 required repetitive detailed inspections for discrepancies (including finish damage, corrosion, pitting, and base metal scratches) of the transition radius of the left and right MLG trunnion pins, and corrective action if necessary. Replacing or overhauling the trunnion pins terminates the actions required by AD 2009-24-07. This new AD adds airplanes to the applicability of AD 2009-24-07. This AD was prompted by reports of corrosion protection damage to the forward trunnion pin on additional airplanes. We are issuing this AD to prevent stress corrosion cracking of the forward trunnion pins, which could result in fracture of the pins and consequent collapse of the MLG.

We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 747 airplanes. This AD was prompted by reports of cracking in particular areas of the bulkhead structure at body station (BS) 2598. This AD requires repetitive inspections, including post-repair and post-modification inspections, for cracking in the bulkhead structure at BS 2598; certain one-time inspections of certain fasteners and support frame modifications on certain airplanes; related investigative and corrective actions, if necessary; and an interim modification that would terminate certain repetitive inspections. We are issuing this AD to detect and correct fatigue cracking of the BS 2598 bulkhead structure, which could adversely affect the structural integrity of the bulkhead and the horizontal stabilizer support structure, and result in loss of controllability of the airplane.

This action proposes to establish a new policy that would consider the impact of one engine out procedures in the aeronautical study process conducted under existing 14 CFR part 77 criteria when the airport operations potentially affected by a determination of no hazard are able to use a dedicated one engine out flight path. Additionally, this proposed policy statement notes that the FAA has the authority to consider the cumulative effects of construction in concentrated areas when evaluating the potential for a hazard to navigation.

This action prohibits certain flight operations in a portion of the Simferopol (UKFV) Flight Information Region (FIR) by all U.S. air carriers; U.S. commercial operators; persons exercising the privileges of a U.S. airman certificate, except when such persons are operating a U.S.-registered aircraft for a foreign air carrier; and operators of U.S.-registered civil aircraft, except when such operators are foreign air carriers. The FAA finds this action to be necessary to prevent a potential hazard to persons and aircraft engaged in such flight operations.

We are revising an earlier proposed airworthiness directive (AD) for certain The Boeing Company Model 757-200 and -200PF series airplanes; and Model 767-200 and -300 series airplanes. The NPRM proposed to require doing an inspection to determine the part number and serial number of the hub assembly of the ram air turbine (RAT), and replacing the hub assembly of the RAT with a new, serviceable, or reworked and re-identified hub assembly if necessary. The NPRM was prompted by reports indicating that the counterweights in some hub assemblies of the RATs could be under strength and fracture when the RAT is rotating. This action revises the NPRM by adding airplanes to the applicability; adding an additional part number and serial number inspection to determine if certain RAT hub assemblies are installed; and, for affected RAT hub assemblies, doing an inspection for missing and fractured balance washer screws, and replacement if necessary to address an additional defect identified within the RAT hub assembly. We are proposing this supplemental notice of proposed rulemaking (SNPRM) to prevent an inoperative RAT, which, following a dual engine shutdown in flight, will cause loss of all hydraulic power to the primary flight controls, resulting in subsequent loss of control of the airplane. Since these actions impose an additional burden over that proposed in the NPRM, we are reopening the comment period to allow the public the chance to comment on these proposed changes.

This action establishes Class E Airspace at Nashville, TN, to accommodate a new Area Navigation (RNAV) Global Positioning System (GPS) Standard Instrument Approach Procedure (SIAP) serving Nashville International Airport. This action enhances the safety and management of Instrument Flight Rules (IFR) operations at the airport.

This action amends Class D and Class E Airspace, and establishes Class E airspace at Tri-Cities Regional Airport, Tri- Cities, TN. Airspace reconfiguration is necessary to alleviate traffic issues in the surrounding area for Johnson City Airport and Edwards Heliport so aircraft can navigate in and out of their respective airports in Visual Flight Rules conditions under 700 feet. This action enhances the safety and airspace management of aircraft within the Tri- Cities, TN area.

This action amends Class E Airspace at Greenville, ME, as the Squaw Non-Directional Beacon (NDB) has been decommissioned, requiring airspace redesign at Greenville Municipal Airport. This enhances the safety and management of aircraft operations at the airport. This action also updates the geographic coordinates of the airport.

We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 747-100B SUD, 747-200B, 747-300, 747- 400, 747-400D series airplanes. This proposed AD was prompted by an evaluation by the design approval holder (DAH) indicating that the upper deck tension ties are subject to widespread fatigue damage (WFD). This proposed AD would require repetitive inspections for cracking in the upper deck tension ties, and related investigative and corrective actions if necessary; tension tie replacement; and post-replacement repetitive inspections for cracking in the upper deck tension ties, and related investigative and corrective actions if necessary. We are proposing this AD to detect and correct fatigue cracking of the upper deck tension ties. Severed or disconnected tension ties at multiple locations could result in rapid decompression and loss of structural integrity of the airplane.

This action proposes to establish Class E airspace at Memphis, MO. Controlled airspace is necessary to accommodate new Standard Instrument Approach Procedures (SIAP) at Memphis Memorial Airport. The FAA is taking this action to enhance the safety and management of Instrument Flight Rules (IFR) operations for SIAPs at the airport.

We are adopting a new airworthiness directive (AD) for British Aerospace Regional Aircraft Jetstream Series 3101 and Jetstream Model 3201 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as inadequate instructions for inspection for corrosion on the rudder upper hinge bracket and certain internal wing and drainage paths. We are issuing this AD to require actions to address the unsafe condition on these products.

We are adopting a new airworthiness directive (AD) for Ballonbau W[ouml]rner GmbH Models NL-280/STU, NL-380/STU, NL-510/STU, NL-640/STU, NL-840/STU, and NL-1000/STU balloons. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as current inspection intervals are no longer adequate to ensure timely detection of deterioration or damage. We are issuing this AD to require actions to address the unsafe condition on these products.

The Federal Aviation Administration (FAA) is announcing its intent to prepare an Environmental Assessment (EA) pursuant to the National Environmental Policy Act (NEPA) of 1969 and its implementing regulations for the application by Paulding County Airport Authority (PCAA) for certification of Paulding Northwest Atlanta Airport (PUJ) under 14 Code of Federal Regulations Part 139. The EA will also address connected actions related to the introduction of scheduled commercial air carrier service at PUJ. The purpose of the EA is to consider and evaluate the potential environmental impacts of the proposed actions and alternatives, including the no-action alternative.

The Federal Aviation Administration (FAA) announces its determination that the updated noise exposure maps submitted by the Indianapolis International Airport (IND) under the provisions of 49 U.S.C. 47501 et. seq (Aviation Safety and Noise Abatement Act) and 14 CFR part 150 are in compliance with applicable requirements.

This action amends Class E airspace at Paragould, AR. Decommissioning of the Paragould non-directional radio beacon (NDB) at Kirk Field Airport has made reconfiguration necessary for standard instrument approach procedures and for the safety and management of Instrument Flight Rule (IFR) operations at the airport. Geographic coordinates are also updated.

The Federal Aviation Administration (FAA) published in the Federal Register of May 3, 2013 a document amending the design requirements in the airworthiness standards for transport category airplanes to minimize the occurrence of design-related flightcrew errors. This document corrects an inadvertent amendment number that appears in the heading of the publication of that final rule.

We propose to adopt a new airworthiness directive (AD) for certain the Boeing Company Model DC-9-10, DC-9-20, DC-9-30, DC-9-40, and DC-9-50 series airplanes. This proposed AD was prompted by an evaluation by the design approval holder (DAH) indicating that the bulkhead dome tees, which connect the bulkhead web to the fuselage, are subject to widespread fatigue damage (WFD). This proposed AD would require repetitive inspections of the improved ventral aft pressure bulkhead tees and replacement if necessary. We are proposing this AD to detect and correct fatigue cracking of the bulkhead dome tees, which could result in reduced structural integrity and rapid decompression of the airplane.